TTH Aviation. Brief TTH Soviet aircraft. Main characteristics Su-34

The painting of La-7 aircraft painting La-7 did not differ from the camouflage of other fighters of that period. According to the joint order of the NCAP and BBC KA No. 389c / 0133 of July 3, 1943, all the fighter aircraft from the summer of the same year received a new standard masking color. Top I.

The painting of La-9 aircraft as mentioned above, the first experienced La-9 was built at factory No. 21 in early 1946. The plane had a one-color color of all surfaces, it was probably the gray-blue Aerolac AMT-11. On the plane allocated only shiny unpainted

The color of La-11 aircraft painting La-11 fighters differed not much from La-9. The evolution of this color is well illustrated by the following table, representing the consumption of the main paints and varnishes for the manufacture of one La-11 at factory No. 21: all external surfaces

The creator of fire aircraft in 1937 at the aviation festival in Tushino above the heads of the audience, a completely unusual aircraft swept. The airplane did not have a tail - only wide wings that were painted with red feathers, which made a plane look like a fabulous

The creator of high-rise aircraft on August 23, 1943 from the headquarters of the Western FRONT air defense to the commander of Artillery N.N. Voronov and People's Commissar A.I. Shahurin came the report: "On August 22, 1943 from 08 hours 40 minutes to 10 hours and 10 minutes, the opponent made an intelligence in Moscow and the surrounding

SU-25 - Soviet / Russian armored subsonic attack aircraft designed to support land forces over the battlefield Day and at night with the direct visibility of the goal, to destroy objects with specified coordinates around the clock in all weather conditions. In the Russian and Ukrainian troops received the nickname "Grache".

Su-25 (T-8 product, NATO: Frogfoot)

The aircraft took off for the first time on February 22, 1975. These aircraft are operated since 1981, participated in a variety of military conflicts. Airplanes will be in the ranks of Russia Air Force at least until 2020. In 2009, the Ministry of Defense of the Russian Federation announced the renewal of the procurement of attack aircraft of this type for the Russian Air Force.

History

Work on the creation of SU-25 began in OKB P. O. Dry in the mid-70s in an initiative basis, when it became clear that the decision taken in 1956 on the abolition of assault aviation and the transfer of its functions to the bombers fighters is erroneous. The head designer SU-25 was the former Tank T-34 commander, one of the best aircraft designers of the XX century, Oleg Sergeevich Samoilovich (1926-1999).

When developing an attorney, research and development work on 40 topics were manufactured, about 600 samples and layouts were made and tested. In February 1975, the prototype of the attack aircraft, which received the working designation T-8, took off, and in 1980, the Stormsovik was adopted by the USSR Air Force under the designation of the Su-25. In 1981, the SU-25 squadron consisting of 12 cars has already participated in hostilities in Afghanistan.

Design

Engines

SU-25 engines are located on both sides of the fuselage in special motogondals at the place of pairing the wing with the fuselage. The engines are equipped with an unregulated nozzle and air intake. The interremmer resource is 500 hours.

Early versions of the SU-25 were equipped with two unfaffolding single-circuit turbojet engines P-95Sh rod 4100 kgf each. The engines had an average specific fuel consumption of 1.28 kg / kgf hour, as well as autonomous electrical launch.

Later on the attack aircraft began to establish more perfect R-195 with an increased to 4300 kgf tight. R-195 engines for a long time were secret, in particular, in the airplane in France in 1989, the T-8-15 aircraft P-195 engines were replaced by R-95Sh. The design was strengthened compared to the prototype R-13. The engine is able to withstand a direct hit of a 23 mm projectile and retains its performance with numerous less serious damage. It was also reduced by IR radiation, which makes the aircraft less vulnerable to rockets with infrared heads of homing.

The P-95 and R-195 engines were recognized as the most reliable in their class.

Much attention is paid to the survivability of the design and screening of systems with the settlement so that one hitting means of the defeat it was impossible to deal with both engines. When withdrawing a single engine, the aircraft can continue the flight on the other.

The main fuel for these engines is aviation kerosene. The engines are supplied with fuel from 4 built-in tanks (2 in the fuselage, one by one in each of the semi-cerebrals) with a total volume of up to 3660 liters, and suspension is allowed to 2 suspended fuel tanks (PTB-800) The capacity of each 840 liters. Thus, the total volume of fuel tanks can be up to 5300 liters.

Protection, Life System and Salvation System

Su-25 is a highly disgraced aircraft, a combat survivability system accounts for 7.2% of the normal take-off mass or 1050 kg. Vital stormcut systems are duplicated and shielded less important.

Very much attention is paid to the protection of critical assemblies and elements - the pilot cabins and the fuel system.

The pilot cab is made welded from ABT-20 Aviation Titanium. The thickness of the armored is from 10 to 24 mm. The windshield provides anti-optical protection and is a glass of 55 mm thick. Behind the pilot is protected by armored aircraft made of steel 6 mm thick. The pilot is almost completely protected from the shelling from any hard weapon with a caliber of up to 12.7 mm, and at the most dangerous directions - caliber up to 30 mm.

In case of critical damage to the aircraft, the safety and rescue of the pilot is provided by the K-36l catapult chair, which ensures the salvation of the pilot in all modes, speeds and altitudes of the flight. Before catapults, the cab lamp is discarded. Catapultation management is carried out manually using control handles for which you need to pull with both hands.

Armament

Su-25 is equipped with a powerful set of weapons - aircraft, airbags of various caliber and destination, managed and unmanaged air-earth missiles, controlled air-air missiles. In total, 32 types of weapons can be installed on Su-25. The attachment possesses the built-in 2-bodily 30-mm aircraft gun GS-30-2, the rest of the armament is placed on the aircraft depending on the type of tasks set. The aircraft is equipped with 10 point of the suspension of additional weapons and cargo (5 under each half-liter). For the air-surface suspension, BDZ-25 pylons are used, and for suspension controllers (UR) "air-air" - APU-60 (aviation pads).

Artillery arms

The attack aircraft is armed with VPU 17A (built-in cannonal installation) with a double-barreled 30-mm aircraft of GS-30-2 (Grau 9A623 index), made according to the gasta scheme. Airstrike is designed to defeat armored vehicles, the living force of the enemy, as well as air targets on medium and close distances. The gun is relatively compact for instruments of such raininess and caliber: the length of the barrel is 1.5 m, and its mass without a wip is 105 kg. The GS-30-2 is fixed by a fixedly relative to the glider, the guidance is carried out by maneuvering the aircraft. Power guns - tape. The shooting control is carried out by means of electroclacial, using a 24 volt direct current. The complete ammunition is 250 ammunition, and the aircraft can be consumed by the entire wiping of one continuous queue. The trunk allows you to produce up to 4,000 shots without deterioration. The initial speed of the projectile is 900 m / s. The shooting pace of this aircraft is 3000 shots per minute.

The gun can fire the following types of ammunition:

Fragantive-fuke-in-war OPZ-30 projectile,
- Skolk-fuke-in-war tracer projectile OFZT-30,
-Bronet-discontinuous projectile BR-30,
- Mem-elementary projectile ME-30.
- Also, it is possible to install on the Su-25 additional artillery armament in the form of suspended cannon containers SPTU-22-1, each of which is equipped with a two-sliced \u200b\u200b23-mm gun of GS-23, made according to the gasta scheme. The ammunition of each cannon container is 260 ammunition. Up to 4 such containers can be installed on the aircraft.

Unmanaged air bombs

In the base version, the Su-25 can use the following unmanaged air bombs:

Fab-100 one or four bombs (using MBD2-67U) on the suspension
-Fab-250
-Fab-500
-Sab-100
-Betab-500
-Betab-500shp
-RBK-250
-Rbk-500.
-KMGU-2.
-SB-500
-Dab-500p

Unmanaged rocket weapons (NAR)

Su-25 can use blocks of NAR with the following rockets with various BC (combat part):

C-5
-S-8.
-S-13
- On one on the suspension:
-S-24B.
-S-25

High-precision bombs and rockets

To use the controlled weapon of the air-surface class, the Su-25 (as well as the Su-17m4) is equipped with a laser rangefinder-padded indicator (LD) "Maple-PS". After capturing the target and start, the pilot rocket should highlight the goal before its defeat. Due to the location of LDs in the nasal part of the aircraft, the viewing angle is sent to the front hemisphere, and not to the bottom, which is why controlled airbabs does not use the SU-25 basic modification. Controlled rockets:

C-25L.
-H-25ml
-H-29l

Air-air weapon

For self-defense and combating helicopters, the Su-25 is equipped with two controlled R-60 rockets of a small radius of action with IR homing heads. Rockets are attached to APU-60 aviation launchers placed under the wing.

Since the R-60 rockets have already been discontinued, and their storage time ends, then when modernizing the SU-25 Air Force aircraft to the Su-25 cm and Su-25cm version, pylons intended for the APU-60 launchers are dismantled. At the upgraded SU-25CM attack aircraft, R-73 missiles are used, the PU (starting device) of which is suspended to extreme BDZ-25 holders.

Navigation and accessories

BKO "Talisman" - an onboard defense complex for individual protection of combat aircraft from managed missiles.

Modifications

SU-25-battle single attack aircraft

Su-25K (commercial) is the export version of the Su-25. 180 cars are built in the 1984-1989. Su-25k also called the project of the shutture vehicle of the attack aircraft.

Su-25T-designed in 1984 based on SU-25UB anti-tank attack aircraft. The central section has strengthened, in the girling instead of the second cabin, radio-electronic equipment is placed, the nasal part is changed, the aiming complex and-251 "flurry" is added, an ILS is installed, as well as the ability to use modern high-precision ammunition, hermetic cabin.

SU-25UB-training double attachment. It is in service with Georgian Air Force.

Su-25SM- upgraded combat single attack aircraft. Avionics updated (from aviation and electronics, it is also brao - onboard radio-electronic equipment), Ils added (indicator on the windshield glass - a system of aircraft, designed to display symbolic navigation and special information on the windshield, on the background of a typical situation. Using ILS It makes it possible to largely reduce the likelihood of the information overload of the pilot, forced to monitor both the surrounding space and the testimony of numerous instruments. This technology originally designed exclusively for military aviation (primarily for jet fighters and helicopters), is currently being used in civil aviation and automotive industry.) and MFD (multifunctional indicator / display (eng. Multi-Functional Display - MFD) - a common term for a multi-mode device for displaying various service graphics and tele-information in the cabin cabin, issued onboard Systems and sensors. Information display modes can switch both automatically and manually by the pilot (operator). Single-mode devices, as a rule, have more specified names, such as the "tactical setting screen").

SU-25KM- modernized by Israel Georgian attack aircraft. Avionics updated, plus added the possibility of using NATO ammunition.

SU-28- training aircraft. Serially not produced.

Su-25Tugg- training aircraft for training takeoff and landing on the ship deck

Su-39-anti-tank attack aircraft, further development of SU-25T. Equipped with a radar station "Spear-25" in the suspended container.

SU-25BM- upgraded double attack aircraft created as an educational and combat version of the Su-25cm and Su-39. On the aircraft implemented all the developments of previous modifications. The base for the new aircraft was the double SU-25UB. Radioelectronic equipment is complemented by the Barç-2 side equipment complex, and also planned to add "Spear" radar (there is no RLS prototype). It is assumed that the aircraft can be used both as a training for single modifications and as an independent combat unit. Moreover, in the latter case, SU-25UBM will be able to exploration, targeting and coordinating actions, turning into an air team point. The first test flight has made a new aircraft on December 6, 2008 at the Kubinka airfield near Moscow. In 2011, the first stage of the SCS of the aircraft was completed. For the first time, the aircraft will be equipped with a powerful RTR and RES system (radio electronic wrestling), as well as the BCO complex (the onboard defense complex is a means of radio-electronic combat and is intended for individual protection of combat aircraft from the air-air rockets and the "surface-air").

Su-25m1- Ukrainian modernization Su-25. Equipped with upgraded equipment of Ukrainian producers - satellite navigation, a new SVS system (the system of air signals of modern aircraft is a software and hardware system intended for measurement, calculation and issuance to the LA crew and onboard systems (consumers) information about high-speed parameters , as well as other parameters, such as air temperature, attack and slip angles. It consists of a large group of sensors - air pressure receivers (graduaters of static pressure, dynamic pressure or combined full-pressure receivers), sensors of the inverted flow (high-speed pressure) and a number of others Sensors, as well as pressure transmission pipelines (so-called static "with" and dynamic "d" lines), processing devices and conversion, which convert the received information into electrical signals (on which the bulk of the aircraft equipment works). In decentralized CSS on S. S. Amelet has a large group of diverse instruments - kV (height corrector), ICHM (Mach number indicator), KZSP (dashboard corrector), pressure relay measuring complex (ICDDF), etc. A centralized CSA, as a rule, has a single calculator (for example, the central of the speed and height of the CSV), which receives information from the receivers, transforms it into proportional electrical signals and issues consumers. In the decentralized SBS in the crew cabin, aneroid-membrane appliances and pointers are used: heights (for example, VD-20 altimeter), speeds (for example, CB-1500), variometers, etc. In centralized CCS, electrical indicators of speed, height and other flight parameters are used, or information is derived at the MFI. As a rule, even in the most modern digital instrument equipment of the aircraft there is a place for a backup barometric altimeter and a speed pointer connected directly to pressure receivers), an upgraded radio station, a modern trades counter. Analog sight is replaced by digital, which made it possible to increase the accuracy of aiming by approximately 30%. The plane is able to now use standard weapons for ground targets at any time of the day, in conditions of poor visibility and without leaving the clouds. Very substantially, almost 3 times, an increase in the "ceiling" of weapons. Installed module of air parameters and onboard register of digital parameters of the BRCP. Modernized SU-25M1 single attack aircraft are equipped with a new "digital" camouflage. Production on the modernization of the attack aircraft, occurs in Zaporizhia, at the airfield of the State Enterprise "Zaporizhia State Air Requirement Plant".

Su-25ubm1- Ukrainian modernization SU-25UB analogue Su-25 m1.

Combat application

Civil War in Angola (1975-2002)

The Angola Air Force received a small amount of SU-25 in the late 1980s and actively used them against UNITA units during the 1990s.

Afghan War (1979-1989)

In the spring of 1980, four SU-25 took place in Afghanistan a combat rating, showing full superiority over its competitors Yak-38. Since mid-1981, one SU-25 squadron participated in the Afghan conflict, in 1984 it was enlarged before the airmaker. The fighting has discovered high vitality and maneuverability of the attack aircraft. A relatively low speed allowed him to apply very accurate blows, which is usually deprived of fighter-bombers. In Afghanistan, SU-25 got his nickname "Grache", becoming the most famous aircraft of that war. After the appearance of CRKK "Stinger" in 1987, the Stormzovik has undergone modernization in 1987 in order to increase the survivability.

One of the Pilots "Graco" in Afghanistan was Alexander Rutskaya (the future Vice-President of the Russian Federation). During the participation in hostilities, he was twice shot down - in April 1986 by fire from the ground and in August 1988 by the Pakistani fighter F-16.

On average, each shot down SU-25 accounted for 80-90 combat damages, there were cases when aircraft with 150 samplers returned to the base! Most sources talk about the loss in Afghanistan 23 storms of the Su-25 and 8 pilots, while noted that no case of the loss of the aircraft was not recorded due to the explosion of fuel tanks or the death of the pilot (although there is an opinion that the aircraft of Art. Lieutenant Shumihina was Lost as a result of the defeat of the pilot with fire from the ground). Victor Markovsky researcher considers this data incomplete and, referring to the documents of the Air Force Air Force of the 40th Army and the CPs of the Turkway Air Force, informs about the loss of 33 attack aircraft and 12 pilots, noting that in this assessment, he did not take into account several aircraft, written off due to combat and non-combat Damage. In the books of Markov and Ildar Bedgetdinova, as well as in some other sources you can find a description of the circumstances of the loss in Afghanistan 34 attack aircraft (including 24 in the air and 10 on Earth) and the names of 12 dead Pilots Su-25.

Iranian Iraqi War (1980-1988)

Su-25 entered Iraq in the second half of the 1980s. According to one source, they participated in the war very intensively, on others - literally several combat departures. The effectiveness of their application, as well as possible losses, is not known.

War in Persian Gulf (1991)

Iraqi Su-25 did not make a nicerly military departure during this war, but suffered a fighting loss. Seven aircraft flew to Iran, where they were enrolled in local Air Force, two more were shot down by American F-15 fighters during the flight attempt and a certain number was destroyed by NATO airborne on Earth. Total Iraq lost 31 Su-25.

Civil War in Tajikistan (1992-1997)

During the war, SU-25 of the Air Force of Russia and Uzbekistan acted.

Abkhaz War (1992-1993)

Georgia used his SU-25 in the war. Several aircraft were destroyed by the Abkhaz air defense. At least one case of participation in the SU-25 War of Russia is also known.

Karabakh War (1991-1994)

Su-25 was the first combat aircraft who took part in the Karabakh war. In April 1992, the pilot of the Russian Air Force of Russia Azerbaijanis Vagif Kurbanov hijacked his attack aircraft to Azerbaijan and performed the combat departures until he was shot down. Later Azerbaijan received several more aircraft. By the end of the war, Armenia had its own Su-25.

First Chechen War (1994-1996)

Su-25 was the main combat aircraft used by the Russian Air Force in the Chechen conflict. At the very beginning of hostilities, Su-25 attack aircraft destroyed all Chechen aviation on Earth. These aircraft actively acted in winter and in the spring of 1995; In the future, aviation was applied episodically due to the nature of the war after the June truce. The attack aircraft again confirmed their high efficiency. Combat losses amounted to 5 aircraft (four shot downs and one is written off due to combat damage). Despite the high combat survivability of SU-25, one of the aircraft was lost as a result of the death of the pilot from the enemy's fire from a large-caliber machine gun DSHK - bullets punched a unarround side glass of the cabin.

War in Congo (1997-2002)

8 attack aircraft were purchased by the Republic of Congo in 1999. All combat units were made by hired pilots from Russia, Ukraine and Belarus (since there were no prepared pilots in the National Air Force of the Republic of the Republic of the Congo)).

Ethiopian Eritrean Conflict (1998-2000)

Both sides were in service with the Su-25 to the beginning of the third part of the fighting (May-June 2000). It is selected by the use of controlled Rockets X-25 and X-29 by Ethiopian attack aircraft.

Second Chechen War (1999-2000)

As in the first war, the Su-25 was often used to provide direct aviation support to the ground divisions of federal forces, as well as made departures to the "free hunt." Aviation Action Action has sharply decreased after the completion of the main part of the fighting in the spring of 2000. By mid-2001, 6 aircraft were lost.

Other conflicts

Conflict in Macedonia (2001)

Directly during the hostilities of the Macedonia Air Force received several Su-25 from Ukraine and used them for strikes on the positions of Albanians.

French-Ivoire Conflict (2004)

In the afternoon of November 6, the aircraft SU-25 Ivorian Air Force, attacked the position of French peacekeepers, as a result of which 9 people were killed, 31 wounded. A few hours later, French aviation inflicted a retaliatory blow to Jamusukro Airport and destroyed both Côte d'Ivoire Su-25 on Earth.

Armed conflict in South Ossetia (2008)

SU-25 attack aircraft were intensively used by the Air Force and Georgia. During the conflict, officially confirmed losses of the Russian Air Force amounted to three SU-25, four more were quite seriously damaged, which significantly exceeded the loss and damage to the remaining types of used aircraft. South Ossetian and Russian parties at different times were announced to destroy a number of Georgian aircraft.

The War was applied by the Su-25cm, but due to the fact that there were no Rabs on these aircraft, they often fell under the fire of the enemy. An outdated target complex did not allow the aircraft to work in bad meteors, as well as applying the rockets X-25/29 at night, mostly the attack aircraft used drugs and air bombs.

Darfur conflict

According to the International Organization Amnesty International, Sudan has repeatedly applied Su-25 for attacks as a military and civilian objects in Darfur. The attack aircraft were delivered from Belarus in 2008-2010; According to the conditions of the embargo imposed on Sudan, the UN, the weapon supplied to the country should not be used in the hostilities in Darfur.

Armed conflict in the east of Ukraine (from 2014)

Su-25 attack aircraft apply as part of the Air Force of Ukraine during the civil war in the East of Ukraine. As of August 22, 2014, the data confirmed by the Ukrainian side of the loss of aircraft was: 3 units damaged by 3 units destroyed as a result of hostilities. Information about hitting on August 20 Su-25 is erroneous, in fact, according to the information refined by the Council of National Security and Defense of Ukraine, the front-line bomber SU-24M was shot down.

Armed conflict in the north of Iraq (2014)

The Su-25 acquired by Iraq and the Su-25 acquired at the end of June 2014, made the first combat departures on December 25 in the sky above the surroundings of the Iraqi city of Tikrit in the province of Salah-Ed Ding, thereby turning to the Extremist State of the Islamic State of the Extremist Organization

Characteristics (TTX)

Technical characteristics Su-25

Crew: 1 pilot
-Tlin: 15.36 m (with PVD)
-Sima wing: 14.36 m
- High: 4.8 m
- Wing - 30.1 sq.m.
-Ceficiency of the wing elongation: 6
-Ceficient of the narrowing of the wing: 3.38
"Fall-in-grain edge: 20 degrees
- Freight V Wing: -2.5 Grad
- Chassis - 3.57 m
Chassi-Chassis: 2.51 m
-Mass empty: 9315 kg
-Mass is equipped: 11,600 kg
-Normal running weight: 14,600 kg
-Maximum takeoff weight: 17 600 kg
- Fuel mass in the inner tanks: 3000 kg
-Mass armor protection: 595 kg
- Floor: 48.5 kg windshield (armway)
- Pilot - 424.9 kg
- Fuel and oil systems: 121.6 kg
- Treadmage: 160 kg
-Sile installation: 2 x TRD R-95SH
-Theka: 2 x 4100 kgf (40.2 kN)

Fewer characteristics

Maximum speed: 950 km / h (with norms. Battle load)
Cruising speed: 750 km / h
- Speed \u200b\u200bspeed: 210 km / h
Combat radius: 300 km
Practical range: (with norms. Battle load)
-on high:
-Bez PTB: 640 km
-C 4 PBB-800: 1250 km
- Earth:
-Bez PTB: 495 km
-C 4 pb-800: 750 km
Distant distance: 1950 km
Practical ceiling: 7000 m
- Maximum height of combat application: 5000 m
- Viragueradius: 680 m (with norms. Battle load for 1500 m at 555 km / h)
-Scorption: 60 m / s (in the earth with a load of 1000 kg)
-Working on the wing: 485 kg / sq.m. (with norms. takele weight)
-The qualifying: 0.56 / 0.466 (with norms. / Max. Takele weight)
Layout Length:
-No concrete runway: 550 m
-An the groundwall: 600 m
Mileage Length: (without brake parachute)
- on the concrete runway: 600 m
-An the soil runway: 700 m
Maximum operational overload:
- with normal battle load: + 6,5G
- with maximum battle load: + 5,2g

Armament

Rifle-cannon: two-sided 30-mm GS-30-2 gun with ammunition 250 ammunition
Pendant points: 10
Battle load:
-Normal: 1400 kg (4 FAB-250, 2 r-60, ammunition cannon)
-Maximum: 4400 kg
Controlled rockets:
-Arenet "Air-air": 2 x P-60 (AA-8)
-Arenet "air-surface": 4 x x-25ml or x-25mlp or C-25l or 2 x x-29l
Unmanaged rockets:
-256 (8 x 32) x 57 mm C-5 in UB-32 blocks or
-160 (8 x 20) x 80 mm C-8 in B-8 blocks or
-40 (8 x 5) x 122 mm C-13 in B-13 blocks or
-8 x 240 mm C-24 or 266 mm C-25
Bombs: FreeFollow and Corrected Different Appointments, Bomb Cassettes
-8 x 500 kg (Fab-500, RBC-500, etc.) or
-8 x 250 kg (Fab-250, RBC-250, etc.) or
-8 or 32 x 100 kg or
-8 x KMSU-2 containers
Cannon containers: 4 x SPU-22-1 with a two-sided 23-mm gun GS-23 with 260 ammunition

Avionika

Laser reference station: "Maple-PS"
-Mass: 82 kg
- difference in range: + ...- 5 m
-Gollah laser deflection:
- Height:? 30 hail / + 6 degrees
- Azimuth: + ...- 12 degrees
-Conitorial GLONASS navigation system (for Su-25cm)

It consists in arms

Russia: There are about 200 airplanes of this type in the rank and about 100 are still on storage.
-Azerbaijan: 19 Su-25 are delivered from Belarus and from Georgia + 5 Su-25 to be delivered from Ukraine.
Yangola
-Armenia
-Belorussia
-Bulgaria
-Gambia
-Georgia
- Democratic Republic of Congo
-Iraq
-Iran
-Kazakhstan
-Kundra
-Peru
-Sudan
Production
-Yuzbekistan
-Ukraine
-Chad
-Equatorial Guinea
-Erterey
-Ethiopia.

Technical data Yak-1
Crew - 1 person
Maximum take-off mass - 2858 kg
- 8.48 x 10.0 m.
- 1 (M-105P) x 1050 hp
Maximum flight speed: at an altitude of 4,950 m- 578 km / h
Push-power (average) - 14.6 m / s
Practical ceiling - 10,000 m
Range of flight - 700 km
Armament:1 gun 20mm Schwak, 2 machine gun 7,62 mm Case

Technical data LAGG-3
Crew - 1 person
Maximum take-off mass - 3023 kg
Dimensions: Wing Length - 8,81 x 9.8 m.
Power installation: the number of engines x power - 1 (M-105PF) x 1210 hp
Maximum flight speed: at a height of 3,560 m - 591 km / h
Push-power (average) - 11.7 m / s
Practical ceiling - 9600 M.
Range of flight - 650 km
Armament:1 gun 20mm Schwak, 1 machine gun 12.7mm UBS

Technical data MiG-3
Crew - 1 person
Maximum take-off mass - 3300 kg
Dimensions: Wing Length - 8.25 x 10.2 m.
Power installation: the number of engines x power - 1 (AM-35A) x 1350 hp
Maximum flight speed: at an altitude of 7,800 m - 622 km / h
Push-power (average) - 11.7 m / s
Practical ceiling - 12000 M.
Range of flight - 1250 km
Armament:1 Machine gun 12.7mm UBS, 2 machine gun 7.62 mm Case - up to 200 kg or 6-8 RS-82

Technical data I-16
Crew - 1 person
Maximum take-off mass - 1941 kg
Dimensions: Wing Length - 6,13 x 9.0 m.
Power installation: the number of engines x power - 1 (PD M-63) x 1100 hp
463 km / h
Push-power (average) - 0.7 m / s
Practical ceiling - 9700 M.
Range of flight - 700 km
Armament:1 Machine gun 12.7mm UBS, 4 machine gun 7,62 mm Case - up to 200 kg or 6 RS-82

Technical data I-15BIS (I-152)
Crew - 1 person
Maximum take-off mass - 1648 kg
Dimensions: Wing Length - 6.7 x 10.2 m.
Power installation: the number of engines x power - 1 (M-25B) x 750 hp
Maximum flight speed: at a height of 3,500 m - 379 km / h
Push-power (average) - 12 m / s
Practical ceiling - 9800 M.
Range of flight - up to 770 km
Armament:4 machine gun 7.62mm PV-1 (or 2 machine gun 12.7mm UBS) - up to 150 kg (6 x 25 kg)

Technical data I-153
Crew - 1 person
Maximum take-off mass - 1 887 kg
Dimensions: Wing Length- 6.1 x 10.0 m.
Power installation: the number of engines x power - 1 (M-63) x 1100 hp
Maximum flight speed: at an altitude of 5100 m - 427 km / h (on a ski chassis)
Push-power (average) - 16 m / s
Practical ceiling - 10600 M.
Range of flight - 510 km
Armament:4 machine gun 7.62mm wool - up to 200 kg

Technical data IL-2
Crew - 2 people
Maximum take-off mass - 6360 kg
Dimensions: Wing Length - 11.6 x 14.6 m
Power installation: the number of engines x power - 1 (AM-38F) x 1750 hp
Maximum flight speed: at a height of 1200m - 405 km / h
Push-power (average) - 5.5 m / s
Practical ceiling - 6900 M.
Range of flight - 685 km
Armament:2 guns 20mm Schwak, 1 Machine gun 12.7mm UBS, 2 machine gun 7,62mm Case - up to 600 kg or 400 kg and 8-10 RS-82

Technical data PE-2
Crew - 3 persons
Maximum take-off mass - 8 300 kg
Dimensions: Wing Length - 12.6 x 17.6 m.
Power installation: the number of engines x power - 2 (M-105PF) x1210 hp
- 482 km / h
Push-power (average) - 7.5 m / s
Practical ceiling - 7800 M.
Range of flight - 1170 km
Armament:4 machine gun 7.62mm wool, 1 machine gun 12.7 mm UBT - 1600 kg (in overload)

Technical data PE-3
Crew - 2 people
Maximum take-off mass - 8040 kg
Dimensions: Wing Length - 12.6 x 17.6 m.
Power installation: the number of engines x power - 2 (PD M-105x1100 hp)
Maximum flight speed at a height of 3,200 m - 535 km / h
Push-power (average) - 9.2 m / s
Practical ceiling - 8800 M.
Range of flight - 2000 km
Armament:2 guns 20mm Schwak, 2 machine gun 7,62mm wool, 3 machine gun 12.7 mm BS - 700 kg

Tactical and technical characteristics of IL-4:
Dimensions: Wing span - 21.44 m., Length - 14.76 m., Height - 4.10 m.
Wing Square- 66.7 square meters. m.
Mass of the aircraft, kg.
- empty - 6 421
- Normal take-off - 10 055
- Maximum take-off - 12 120
engine's type - 2 PD M-88B, with a capacity of 1100 hp everyone
Maximum speed The Earth is 332 km / h, at a height - 398 km / h.
Practical flight range - 4 000 km.
Practical ceiling- 8 300 m.
Crew - 3-4 people.
Armament: 1x12,7 mm Machine gun BT, 2x7.62 mm machine gun Case. Normal bomb load - 1000 kg, limit - 2500 kg. In the versions of the torpedo room - 1 torpedo weighing 940 kg.

Technical data Sat 2M-103A
Crew - 3 persons
Maximum take-off mass - 7880 kg
Dimensions: Wing Length- 12.27 x 20.33 m.
Power installation: the number of engines x power - 2 (M-103A) x960 hp
Maximum flight speed at an altitude of 4 100 m - 450 km / h
Push-power (average) - 8.8 m / s
Practical ceiling - 9300 M.
Range of flight - 1900 km
Armament:4 machine gun 7,62mm wool - 500 kg (in overload on external suspension + 1000 kg)

Technical data SU-2
Crew - 2 people
Maximum take-off mass - 4700 kg
Dimensions: Wing Length - 10.25 x 14.3 m
Power installation: the number of engines x power - 1 (M-82) x 1700 hp
Maximum flight speed: at an altitude of 5850m - 486 km / h
Push-power (average) - 8.5 m / s
Practical ceiling - 8400 M.
Range of flight - 910 km
Armament:6 machine guns 7.62mm wool - up to 600 kg or 400 kg and 8-10 RS-82

Technical data P-5
Crew - 2 people
Maximum take-off mass - 2 858 kg
Dimensions: Wing Length - 10.56 x 15.30 m.
Power installation: the number of engines x power - 1 (PD M-17F) x 680 hp
Maximum flight speed: 244 km / h
Push-power (average) - 4.9 m / s
Practical ceiling - 6000 M.
Range of flight - 2700 km
Armament:1 Synchronized 7.62mm Machine gun PV-1, Paired machine gun 7.62mm Yes on a ring boat over the back cabin - 400 kg

Technical data U-2 Sun
Crew - 2 people
Maximum take-off mass - 1400 kg
Dimensions: Wing Length - 8.17 x 11.40 m.
Power installation: the number of engines x power - 2 (PD M-11D) x 115 hp
Maximum flight speed: 134 km / h
Push-power (average) - 0.7 m / s
Practical ceiling - 1,500 m
Range of flight - 450 km
Armament:1 machine gun 7,62mm wool - 500 kg

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